Global Patent Index - EP 3415419 B1

EP 3415419 B1 20230802 - LANDING GEAR CONTROLLER

Title (en)

LANDING GEAR CONTROLLER

Title (de)

FAHRWERKSREGLER

Title (fr)

ORGANE DE COMMANDE DE TRAIN D'ATTERRISSAGE

Publication

EP 3415419 B1 20230802 (EN)

Application

EP 18177930 A 20180615

Priority

GB 201709609 A 20170616

Abstract (en)

[origin: EP3415419A1] Disclosed is a landing gear controller (120) to control extension and retraction of a landing gear for an aircraft, the landing gear controller (120) configured to cause, during an aircraft take-off or landing procedure, a landing gear extension and retraction system (110) to perform only a first portion of a landing gear extension or retraction process, on the basis of a status of the aircraft and prior to receiving a command for the landing gear to be extended or retracted. Also disclosed is an aircraft landing gear system (100), a method to extend or retract a landing gear of an aircraft during an aircraft take-off or landing procedure, and an aircraft.

IPC 8 full level

B64C 25/18 (2006.01); B64C 25/16 (2006.01); B64C 25/22 (2006.01); B64C 25/24 (2006.01); B64C 25/26 (2006.01)

CPC (source: CN EP GB US)

B64C 25/16 (2013.01 - EP US); B64C 25/18 (2013.01 - EP US); B64C 25/22 (2013.01 - EP US); B64C 25/24 (2013.01 - EP US); B64C 25/26 (2013.01 - CN EP GB US); G05D 3/10 (2013.01 - US)

Citation (examination)

FR 2875475 B1 20080208 - AIRBUS FRANCE SAS [FR]

Designated contracting state (EPC)

AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DOCDB simple family (publication)

EP 3415419 A1 20181219; EP 3415419 B1 20230802; CN 109131845 A 20190104; CN 109131845 B 20230822; GB 201709609 D0 20170802; GB 2563437 A 20181219; US 11345464 B2 20220531; US 11753151 B2 20230912; US 2018362151 A1 20181220; US 2022258854 A1 20220818

DOCDB simple family (application)

EP 18177930 A 20180615; CN 201810618970 A 20180615; GB 201709609 A 20170616; US 201816009470 A 20180615; US 202217736787 A 20220504